Ground control point assignment and determination system

ABSTRACT

Methods, systems, and apparatus, including computer programs encoded on computer storage media, for ground control point assignment and determination. One of the methods includes receiving information describing a flight plan for the UAV to implement, the flight plan identifying one or more waypoints associated with geographic locations assigned as ground control points. A first waypoint identified in the flight plan is traveled to, and an action to designate a surface at the associated geographic location is designated as a ground control point. Location information associated with the designated surface is stored. The stored location information is provided to an outside system for storage.

CROSS-REFERENCE TO RELATED APPLICATION(S)

This application is a continuation of U.S. patent application Ser. No.15/829,477, filed Dec. 1, 2017, which is a continuation of U.S. patentapplication Ser. No. 15/336,569, filed Oct. 27, 2016, which is acontinuation of U.S. patent application Ser. No. 15/093,511, filed Apr.7, 2016, which claims the benefit of U.S. Provisional Patent ApplicationNo. 62/305,428, filed Mar. 8, 2016, the entire disclosures of which arehereby incorporated by reference.

BACKGROUND

Ground Control Points (GCPs) are used in the generation of theortho-rectified imagery, for instance, acting as tie points in imagesthat tie the images to a real-world coordinate frame (e.g., the surfaceof the Earth). To generate ortho-rectified imagery from a collection ofimages that are to be combined (e.g., stitched) together, GCPs need tobe visible within the collection of images, along with highly accuratelocation information for each GCP. Generally, to collect this locationinformation, a person can travel a desired location and set-up a tripodsystem that includes a survey grade GNSS (e.g., GPS) receiver, andvisually mark a physical area associated with the GCP. Locationinformation (e.g., coordinates) associated with the GNSS receiver at thephysical area are obtained, and stored for use as a GCP.

SUMMARY

In general, one optional innovative aspect of the subject matterdescribed in this specification can be embodied in methods that includethe actions of receiving information describing a flight plan for theUAV to implement, the flight plan identifying one or more waypointsassociated with geographic locations assigned as ground control points;traveling to a first waypoint identified in the flight plan, andperforming an action to designate a surface at the associated geographiclocation as a ground control point; storing location informationassociated with the designated surface; and providing the storedlocation information to an outside system for storage.

Particular embodiments of the subject matter described can beimplemented so as to realize one or more of the following advantages.Ground Control Points (GCPs) can be assigned to geographic locations,and each geographic location can, with limited human interaction, beprepared for later identification as a GCP, along with the accurategathering of location information (e.g., GNSS coordinates) of the GCP.For instance, in contrast to a person spending hours, or days, travelingto each geographic location assigned as a GCP, obtaining locationinformation and preparing the location to act as a GCP (e.g., visiblymarking the location), an unmanned aerial vehicle (UAV) can rapidlytravel to each geographic location and automatically prepare thelocation to act as a GCP. For instance, an unmanned aerial vehicle (UAV)can travel to a particular geographic location, perform an operation,action, at the geographic location (e.g., spray-paint a biodegradablemark on the ground, drop a known visually identifiable marker on theground, and so on) to identify the geographic location as a groundcontrol point, and record a location of the geographic location (e.g., acentroid of the mark or known object). Afterwards, another, or the same,unmanned aerial vehicle can perform a flight plan, such as a job toinspect property, or a structure, for damage, and can gather imagesduring the flight plan that include the GCP. In this way, a largeincrease in time-savings can be obtained by drastically reducing thepreparation time that is generally necessary for a person to performprior to a UAV performing a flight plan. For particular geographiclocations, conventional techniques to prepare the geographic locationsto act as GCPs can be dangerous for persons involved in the preparation.For example, GCPs placed near mines or quarries can require people to belocated near cliffs, dangerous equipment, and so on. This can negate thepossibility, or increase costs and difficulty, of preparing thesegeographic locations, and can violate safety protocols of a governmentalentity or a corporate entity. Using the techniques described herein,geographic locations can be prepared as GCPs without placing people inharm's way, enabling a much broader range of geographic locations to beutilized.

The details of one or more embodiments of the subject matter of thisspecification are set forth in the accompanying drawings and thedescription below. Other features, aspects, and advantages of thesubject matter will become apparent from the description, the drawings,and the claims.

BRIEF DESCRIPTION OF THE DRAWINGS

The disclosure is best understood from the following detaileddescription when read in conjunction with the accompanying drawings. Itis emphasized that, according to common practice, the various featuresof the drawings are not to-scale. On the contrary, the dimensions of thevarious features are arbitrarily expanded or reduced for clarity.

FIG. 1A illustrates an example diagram of an unmanned aerial vehicle(UAV) traveling to a geographic location assigned as a ground controlpoint (GCP).

FIG. 1B illustrates an example diagram of the UAV descending towards ageographic location assigned as GCP.

FIG. 1C illustrates example embodiments of a UAV performing actions todesignate a geographic location as a GCP and obtain location informationassociated with the designated geographic location.

FIG. 1D illustrates an example diagram of a UAV implementing a flight toperform a job.

FIG. 2 illustrates an example user interface for assigning groundcontrol points (GCPs) to geographic locations illustrated in imagery(e.g., satellite imagery).

FIG. 3 illustrates a block diagram of an example cloud system.

FIG. 4 is a flowchart of an example process to designate real-worldgeographic locations as ground control points, and obtain locationinformation at the designated geographic locations.

FIGS. 5A-B illustrate example diagrams of an addition embodiment ofdesignating geographic locations as GCPs, and obtaining locationinformation associated with the designated geographic locations.

FIG. 6 illustrates a block diagram of an example UAV architecture forimplementing the features and processes described herein.

Like reference numbers and designations in the various drawings indicatelike elements.

DETAILED DESCRIPTION

Among other features, this specification describes systems and methodsutilized for assigning geographic locations to act as ground controlpoints (GCPs), and causing each geographic location to be prepared foruse as a GCP including, recording sensor information (e.g., imagery)sufficient to later identify the geographic area (e.g., unique featuresof the area such as a manhole cover) or marking the area (e.g.,spray-painting the area or dropping a marker on the area), and recordinggeographic location information of the geographic area (e.g., GNSScoordinates such as GPS coordinates). In this specification, a groundcontrol point is an accurately surveyed geographic location in areal-world area that can be identified in imagery that includes thegeographic location. The imagery can be combined (e.g., stitchedtogether by a photogrammetry system) and placed in a real-worldcoordinate frame using the accurately surveyed location information(e.g., GPS coordinates) associated with each GCP identifiable in theimagery.

As will be described, an unmanned aerial vehicle (UAV) can include, orbe otherwise connected with, a GNSS receiver, such as a GPS receiver, aReal Time Kinetic (RTK) receiver in communication with GNSS satellitesand a ground-based receiver located within a threshold distance, a PostProcessing Kinetic receiver, and so on. The UAV can receive a flightplan generated by a system (e.g., a cloud system as described below) incommunication with the UAV, or a user device (e.g., a device) of anoperator acting in concert with the UAV, that indicates one or morewaypoints (e.g., geographic locations) assigned as GCPs (e.g., indicatedby a user of the system). The UAV can travel to each waypoint, performan action (e.g., an operation) at the waypoint, such as marking thewaypoint, and record precise geographic location information at thewaypoint (e.g., at a centroid of a marked area).

A user of the system can utilize one or more user interfaces to assignGCPs to geographic locations, and the system can generate a flight planfor the UAV to implement. For instance, as will be described below withreference to FIG. 2 , the system can receive an identification of ageographic area, such as a city block, a house address, geographiccoordinates, and so on, and present imagery (e.g., satellite imagery) ofthe identified geographic area. Within the presented user interface, theuser can select points within the imagery to be assigned as GCPs (e.g.,the user can press on a particular portion of a touch-sensitive screen,mouse-click, and so on). To ensure that the GCPs encompass theidentified geographic area, and specifically sufficiently encompass ageographic area that will be utilized in a subsequent UAV flight plan toperform a job (e.g., a flight plan to inspect for damage of thegeographic area), the system can present information describing thesubsequent flight plan, including waypoints the UAV is to travel to,altitudes at which the UAV is to travel, actions the UAV is to take ateach waypoint (e.g., capture imagery), and so on. In this way, the usercan view a flight plan for an intended use of the UAV, to perform a jobsuch as inspecting a property or structure for damage, and ensure thatGCPs are proximate to the flight plan so as to be included in imagerycaptured by the UAV while performing the job.

In this specification, UAVs include any unmanned aerial vehicles, suchas drones, unpiloted aerial vehicles, remotely piloted aircraft,unmanned aircraft systems, any aircraft covered under Circular 328AN/190 classified by the International Civil Aviation Organization, andso on. For example, various types of UAVs may be used to implement theinventions described herein (for example, a fixed wing airplane,helicopter, a multi-rotor vehicle (e.g., a quad-copter in singlepropeller and coaxial configurations), a vertical take-off and landingvehicle, lighter than air aircraft). A multi-rotor vehicle in a coaxialconfiguration may use the same propeller pitch and diameter propellers,use different pitch and diameter propellers, or variable pitchpropellers. In addition, certain aspects of the disclosure can beutilized with other types of unmanned vehicles (e.g., wheeled, tracked,and/or water vehicles). Specifically, an unmanned vehicle (e.g., aground based vehicle, such as a rover) can be utilized to prepare ageographic location as a ground control point (e.g., described belowwith respect to FIG. 1C).

FIG. 1A illustrates an example diagram of an unmanned aerial vehicle(UAV) 4 traveling to a geographic location assigned as a ground controlpoint (GCP) 10A. FIG. 1A includes an inspection area 2 at which a UAV(e.g., the UAV 4, or a different UAV) is to perform a job (e.g.,identifying and characterizing damage in the inspection area 2, such asdamage to a rooftop of a house 6). To ensure that imagery capturedduring the job can be combined (e.g., stitched together) to generategeo-rectified or ortho-rectified imagery, GCPs (e.g., GCPs 10A-10E) havebeen assigned (e.g., as described in FIG. 2 ) proximate to, or within,the inspection area 2 to ensure that they are included in the imagerycaptured while the UAV performs the job. While the GCP assignment isexplained via an auto-piloted flight plan, the UAV may also be flownmanually to a location, and then an action triggered using a user deviceto obtain a ground control point.

Prior to performance of the job, the UAV 4 travels according to agenerated flight plan (e.g., described in FIG. 2 ) that identifieswaypoints (e.g., coordinates of each waypoint, such as longitude andlatitude) for the UAV 4 to travel to, with each waypoint associated witha GCP. Optionally, the flight plan can include a particular speed atwhich the UAV is to travel between waypoints. As will be described inFIG. 1B, upon reaching vertically above a GCP location (e.g., GCPlocation 10A) at the safe altitude 12, the UAV 4 descends towards thesurface (e.g., ground) on which the GCP was assigned, and performs anaction to designate the surface as a GCP, along with obtaining locationinformation of the designated surface. For instance, the UAV 4 can spraya biodegradable fluid (e.g., paint, foam, and so on) on the surface atthe GCP location 10A to designate the location 10A as a GCP (e.g., markthe surface of the location 10A so its visible in imagery), and obtaingeospatial location information at a centroid of the marked surface. Inthis way, while a UAV is performing a job (e.g., a job to inspect damageof a rooftop of the house 6), the UAV can capture imagery that includesthe created GCPs, each with associated accurate location information.

As illustrated, the UAV 4 is traveling at a particular altitude (e.g.,safe altitude 12) to GCP location 10A. The safe altitude 12 indicates analtitude at which the UAV 4 can safely travel (e.g., free ofobstructions) within the inspection area 2, or within a geofenceidentifying allowable locations of the UAV within a real-worldgeographic area or volume, and which can be indicated by a user in aflight plan (e.g., as will be described in FIG. 2 ). For instance, theinspection area 2 includes a house 6 and trees 8, which can interferewith the UAV's 4 safe trajectory as it travels to the GCP location 10A.Therefore, a user generating a flight plan to travel to indicated GCPscan designate the safe altitude 12 (e.g., using satellite imagery of theinspection area 2, 3D models of the inspection area, and so on).Optionally, the UAV 4 can be equipped with sensors (e.g., distancesensors, visual cameras) to actively monitor and detect upcomingobstructions such that no safe altitude 12 is needed.

The GCPs (e.g., GCPs 10A-10E) are arranged surrounding the house 6, andcan be arranged at particular angles surrounding the house 6 (e.g., 30degrees, 45 degrees, 72 degrees, and so on), which a user can selectdepending on the particulars of a flight plan to perform the job. Forinstance, subsequent to traveling to each GCP, a UAV can perform a jobto inspect the rooftop of the house 6 for damage, and depending on theflight pattern the UAV will follow, the user can prefer to place more orless GCPs proximate to the house 6 to ensure that at least one GCP willbe included in images captured while inspecting the rooftop. The usercan place more GCPs proximate to a geographic area, structure, and soon, that is being inspected in a subsequent job, and less GCPs proximateto areas that are not under inspection or where accuracy is lessimportant. In this way, the user can assign more GCPs to be located neargeographic areas the user is interested in, and can thus set a variableaccuracy when generating geo-rectified imagery obtained duringperformance of the job (e.g., areas with more GCPs will have moreaccurate location information).

Optionally, a nearby operator (e.g., a human operator in wirelesscommunication with the UAV 4 utilizing a user device) can modify one ormore geographic locations assigned as GCPs. For instance, the operatorcan visually determine that, for example, GCP location 10D is within athreshold distance of a tree 12, and can modify the GCP location 10D tobe further from the tree 12. As an example, the operator's user devicecan present imagery (e.g., satellite imagery) of the inspection area 12,and the operator can interact with the imagery to assign a differentgeographic location as an updated GCP location 10D. An example userinterface for assigning geographic locations as GCPs is described below,with respect to FIG. 2 .

FIG. 1B illustrates an example diagram of the UAV 4 descending towards ageographic location assigned as GCP 10A. As illustrated, the UAV 4 hastraveled to the GCP location 10A at the safe altitude 12, and is readyto descend towards the surface (e.g., the ground) to perform an actionto designate the geographic location as a GCP, and obtain locationinformation of the designated geographic location. Performing an actionto designate a geographic location as being a GCP (e.g., marking thelocation, recording unique identifiable features of the geographiclocation), and obtaining location information, are described furtherbelow, with reference to FIG. 1C.

Optionally, the UAV 4 can travel to a location vertically above the GCPlocation 10A, and hover until receiving confirmation from a nearbyoperator (e.g., a human operator utilizing a user device in wirelesscommunication with the UAV 4) to descend. In this way, the operator canhave control over the UAV 4 as it removes itself from the safety of thesafe altitude 12, and descends towards potential obstacles and humanpopulation. Additionally, as the UAV 4 descends it might travel out ofview of the operator (e.g., behind the house 6), and the operator canprovide confirmation for the UAV 4 to descend upon the operator movingto a different location that affords constant line-of-sight with the UAV4.

The UAV 4 descends until reaching a threshold distance above the surface(e.g., ground), with the threshold distance being based on a specificaction the UAV is to perform. Optionally, the UAV 4 can descend and landon the surface. As will be described in FIG. 2 , a user can assigngeographic locations as being GCPs for the UAV 4 to travel to, and canindicate specific types of actions the UAV 4 is to perform to designateeach geographic location as a GCP. For instance, the user can indicatethat the UAV 4 is to spray a fluid (e.g., a visible fluid) on thegeographic location (e.g., create a sprayed circular area on thegeographic location), or that the UAV 4 is to carry and deposit (e.g.,place, or drop from a distance) a marker (e.g., an object of a knownshape that can be identified, or that the marker has patterns displayedon the marker), or that the UAV 4 is to obtain detailed imagery of thegeographic location for later use in identifying the geographic locationwithin captured imagery (e.g., certain geographic locations can includeunique features, or capture imagery of sufficient detail, such that thefeatures can be identified in later captured images).

For an action to spray a fluid at the geographic location, the UAV 4 candescend to a threshold distance above the surface at which it canmanipulate a fluid spraying system to spray the surface with a knownshape. For instance, the UAV 4 can hover at the threshold distance andmanipulate a fluid spraying system to spray a circle or sphere of aparticular radius. Additionally, for an action to deposit a marker, theUAV 4 can optionally land on the surface, place the marker, and ascendupwards. Alternatively, for the action to deposit the marker, the UAV 4can descend to a threshold distance above the surface (e.g., a distancesufficiently close to the surface such that the marker falls straight tothe surface without movement during descent or upon landing), and thendrop the marker. Ideally the fluid sprayed is biodegradable andnon-toxic to humans, animals and plants.

FIG. 1C illustrates example embodiments of a UAV performing actions(e.g., operations) to designate a geographic location as a GCP andobtain location information associated with the designated geographiclocation. As described above, each action illustrated in FIG. 1C can beselected by a user generating a flight plan to assign GCPs to geographiclocations, and can be provided to a UAV to implement. The selections candepend on capabilities and configuration information of the UAV, forinstance whether the UAV can spray a fluid, can drop a marker, and soon.

A first embodiment illustrates the UAV 4 creating an identifiable markon a surface (e.g., ground) at a geographic location to designate thelocation as GCP. As illustrated, the UAV 4 is spraying a fluid 20 (e.g.,paint, such as biodegradable visible, infrared, ultraviolet, paint of aparticular color, foam, string, and so on) on the surface to create amarked area (e.g., circular, or any arbitrary polygon shape). The UAV 4creates the identifiable mark while hovering at a threshold distanceabove the surface, and can create the mark utilizing a spray nozzle, orother fluid spray system, connected, or included in, the UAV 4. Forinstance, the UAV 4 can create a circular mark by rotating the spraynozzle in a circular fashion). In this way, a centroid of the createdmark can be identified as being vertically down from the spray nozzle.Alternatively, the UAV 4 can spray the fluid in a direction partiallyhorizontally from the UAV 4, and as will be described, can determine acentroid of the created mark by moving horizontally to the centroid.Other shapes and patterns may be created, for example, x-pattern,cross-hatched, etc. Additionally, the identifiable mark may be createdwith multiple colors, for example, a white sold circle, with a brightorange inner circle.

After creating the identifiable mark, the UAV 4 obtains locationinformation at a centroid of the created mark. The UAV 4 can obtain anoffset (e.g., horizontal distance) from a GNSS receiver to the spraynozzle, and can utilize this offset to accurate determine locationinformation (e.g., longitude and latitude coordinates) of the centroidof the created mark. Additionally, the UAV 4 can capture imagery of thecreated mark, and determine a centroid of the mark using computer visiontechniques. For instance, the UAV 4, or a user device in wirelesscommunication with the UAV 4, can obtain imagery of the created mark,identify boundaries of the mark (e.g., identify an edge of the mark),and determine a centroid inside the boundaries. To determine locationinformation, the UAV 4 can position a center of the camera verticallyover the centroid and obtain location information (e.g., coordinates) atthe centroid, or the UAV 4 can utilize a field of view of the cameraalong with a distance of the UAV 4 to the surface (e.g., using a Lidar,Leddar, sensor, barometric reading, and so on) to extrapolate locationinformation at the centroid. Since the camera capturing imagery islikely to be at a horizontal offset from the GNSS receiver, the UAV 4can utilize the offset when determining the centroid of the created mark(e.g., if the camera is vertically over the centroid, the offset can besubtracted or added to the coordinates).

Optionally, the UAV 4 can ensure that when creating the identifiablemark 20, the mark is created on a substantially flat surface (e.g., adistance from the surface to the UAV 4 at all points within the mark 20are within a threshold variance of each other). In a subsequent flightplan to perform a job, if the surface is not substantially flat, a UAVimplementing the subsequent flight plan can obtain imagery of thecreated mark 20 at different perspectives, with each perspectiveincluding a different centroid of the mark 20. For instance, of the UAVcreates the identifiable mark 20 on an ant hill, a portion of theidentifiable mark 20 can be hidden behind the ant hill depending on aperspective of the UAV implementing the subsequent flight plan.Consequently, the UAV 4 can utilize one or more sensors (e.g., distancesensors such as Lidar, or computer vision techniques of captured imageryduring the UAV's 4 descent) to identify a substantially flat surface,and create the mark on the substantially flat surface.

Optionally, if there isn't a substantially flat surface to create themark 20, or in implementations where the UAV does not identifysubstantially flat surfaces, information describing a shape of thecreated mark 20 can be stored by the UAV 4 in addition to locationinformation. Imagery captured by a UAV implementing a subsequent flightplan to perform a job can therefore include the created mark 20 atdifferent perspectives. A system (e.g., a photogrammetry system)processing the captured imagery to generate geo-rectified imagery canutilize the stored information describing a shape of the created mark 20to extrapolate where in the image the location of the centroid is. Forinstance, if only a portion of the created mark 20 is visible in animage, or if the created mark 20 is distorted due to height variationsof the surface, the system can utilize the shape information todetermine a centroid of the created mark 20 in the image. Since thesystem has access to location information of the centroid, the systemcan accurately place the created mark in a real-world coordinate frame.

The UAV 4 can include, or be connected with, a frame that houses one ormore receptacles for receiving one or more fluid containers (e.g.,biodegradable spray paint canisters), which can be held in place withtension (e.g., spring tension). The UAV used with the frame ideally is amulti-copter UAV with at least 3 arms extending from the body of theUAV. The UAV may have one motor and a rotor for each arm, or a coaxialconfiguration with two motors each with a rotor. The frame ideally isconstructed of a light weight material, such as aluminum or carbonfiber. The frame can be attached to the UAV on the body of the UAV. Anactuator controlled by the UAV computer system may be used to cause thecontainers to release or spray fluid.

The UAV 4 can include fluid containers that dispense fluids of differingcolors (e.g., colors such red, green, blue, or cyan, yellow, magenta,and black.) The fluid may be in a visible light spectrum, or non-visiblelight spectrum (such as ultra-violet, or infra-red). The UAV 4 maycreate identifiable marks 20 of differing colors, enabling a subsequentUAV flight to capture imagery and easily identify the marks 20 (e.g.,the UAV 4 can store information describing the created mark, such ascolor, pattern, and so on, along with recording location information).As an example, marks 20 with a threshold distance of each other can becreated with different colors, enabling an outside system (e.g., aphotogrammetry system) to easily distinguish between the marks 20. TheUAV 4 (e.g., the UAV primary processing system 600) can trigger eachfluid container to create the identifiable mark 20 (e.g., as describedabove). Optionally, the UAV 4 each fluid container can be connected withactuators, which the UAV 4 can trigger to create the identifiable mark20. Furthermore, as will be described, a UAV performing a subsequentflight can spray a solvent (e.g., water, non-toxic biodegradablesolution) to disperse, remove, and so on, any created mark 20. The UAVcan utilize the recorded location information to travel to each createdmark 20 (e.g., at a safe altitude), descend towards the created mark 20,and dispense the solvent.

In a second embodiment, the UAV 4 can carry a physical marker 22 (e.g.,a thin circular puck, a square object, a rectangular object, and so on),and drop the marker 22 on the surface from a threshold distance abovethe surface while hovering, or descend all the way to the surface, anddeposit the marker while not hovering. To determine location informationof a centroid of the marker 22, the UAV 4 can utilize an offset from acenter of a claw, magnet, such as an elector-magnetic that can beswitched on or off, or other grabbing device, or system, oralternatively from a center of the marker 22 while in flight, from theGNSS receiver, to identify location information at a centroid of themarker 22. Furthermore, as described above, the UAV 4 can captureimagery of the marker 22, and utilizing computer vision techniques, candetermine a centroid of the marker 22.

Similar to the created mark 20, the UAV 4 can place the physical marker22 on a substantially flat surface, so that the physical marker 22 isviewable from any perspective. In addition to placing the physicalmarker 22 on a substantially flat surface, the UAV 4 can ensure that thephysical marker 22 isn't placed in water (e.g., a puddle, a pool). Forinstance, the UAV 4 can utilize sensors, such as infrared sensors (e.g.,cameras with wavelength sensitivity of 1.5 to 1.6 micrometers, or 0.9 to1.7 micrometers, and so on), to identify water (e.g., water can appeardark in infrared imagery). Additionally, the UAV 4 can utilizepolarization information to, in part, identify water (e.g., lightreflected from water can be partially linearly polarized, andpolarization phases can be more similar than from other imaged areas).The UAV 4 can also utilize other computer vision techniques, such asdetermining features and local descriptors associated with water, andthen identifying water using the computer vision techniques.Additionally, as will be described, the physical marker 22 can include adisplay (e.g., an LED panel, one or more lights, a display screen, andso on) such that the physical marker 22 can display one or more patternswhich are recognizable to the UAV 4. Similar to the created mark 20, thephysical marker 22 can display different LED patterns when withinthreshold distances of other physical markers 22. For example, patternscan include particular color patterns, shapes, numbers, letters,objects, figures, and so on. In this way, during a subsequent flight,the physical marker 22 will be recognizable in captured images.Additionally, each placed physical marker 22 can be later retrieved by aUAV. That is, the UAV can travel to the location of each physical marker22, and retrieve the physical maker (e.g., the UAV can utilize a claw, amagnet, and so on), to remove the physical marker. Additionally,multiple UAVs can act in concert, with each UAV retrieving one or morephysical markers. Optionally, the UAV retrieving physical markers can belarger in size, or be specially equipped, such that the UAV can retrievemultiple physical markers in a single flight.

As described above, the physical mark 22 is, in some implementations,preferably placed on a substantially flat surface (e.g., a surface whichincludes height variances less than a threshold). To ensure that thephysical marker 22 is placed on a substantially flat surface, the UAV 4utilize one or more sensors that can measure distance (e.g., Lidar,Leddar) and can determine a particular surface to place the physicalmarker 22. As an example, the UAV 4 can measure distances from thesurface to the UAV 4 (e.g., while hovering at a same altitude) at athreshold number of locations (e.g., 3, 4, and so on) included in thesurface, and determine whether the measurements are within a thresholdvariance of each other. The threshold number of locations can beincluded in a polygonal shape of the surface that conforms to afootprint of the physical marker 22. For instance, if the physicalmarker is a puck (e.g., as illustrated), the UAV can measure locationswithin an ellipse of a size at least the size of the footprint of thepuck (e.g., a threshold number of locations spread around inside theellipse). Additionally, if the UAV determines that a portion of themeasured locations are substantially flat with respect to each other,while one or more other measured locations of the surface are greaterthan a threshold distance further, or closer, to the UAV, the UAV canmove horizontally to exclude the one or more other measured locationsand include the portion of locations. That is, the UAV can determinethat a substantially flat surface might exist if it moves horizontallyin the direction of the substantially flat measured locations.

Furthermore, after the physical marker 22 is placed on a surface, theUAV 4 can determine whether the physical marker 22 is level (e.g.,substantially flat, such as substantially horizontal). The UAV 4 candetermine a boundary of the physical marker 22, and utilizing one ormore distance sensors (e.g., as described above), measure distances fromthe physical marker 22 to the UAV 4 (e.g., while hovering at a samealtitude). If the UAV 4 determines that the physical marker 22 is notsubstantially flat (e.g., a particular portion of the physical marker 22is higher, or lower, than other portions at greater than a thresholddistance), the UAV 4 can retrieve the physical marker 22. Afterretrieving the physical marker 22, the UAV 4 can determine asubstantially flat surface (e.g., as described above), and place thephysical marker 22 (e.g., and use distance sensors to determine that thephysical marker 22 is substantially flat).

Optionally, the physical marker 22 can include sensors, such as gyros,magnetic sensors (e.g., compasses), and so on, to actively determinewhether the physical maker 22 is level. As will be described, thephysical marker 22 can communicate with the UAV 4 (e.g., usingBluetooth), and can provide information to the UAV 4 indicating whetherthe physical maker 4 22 is level. The UAV 4 can retrieve the physicalmaker 22 upon receiving information indicating that the physical marker22 is angled at greater than a threshold. Optionally, after the UAV 4places the physical marker 22, the UAV 4 can hover until receivingconfirmation that the physical marker 22 is level, enabling the UAV 4 tomore easily retrieve the physical marker 22 should the need arise.Additionally, the physical maker 22 can include mechanical features onthe bottom of the physical marker 22 that can level the physical marker22. For instance, the physical marker can include self-actualizing legson the bottom that can ensure the maker 22 is stable.

A size of the physical marker 22, or created mark 20 described above,(e.g., radius, width and length) can depend on an altitude at which asubsequent flight plan to perform a job will take place at. Forinstance, if a UAV is subsequently going to travel at a relatively highaltitude from the physical marker 22 (e.g., 50 meters, 60 meters), thephysical marker 22 can be larger than if the UAV is going to travel at alesser altitude (e.g., 10 meters, 20 meters). The specific size canfurther depend on capabilities of a camera that will be included in theUAV performing the job. For example, the resolution of a sensor includedin the camera, focal length of a lens of the camera, aperture of thelens (e.g., if the camera is focusing on an object a distance above thephysical marker 22, a lens with a wider aperture will cause the physicalmarker 22 to be more out of focus), and so on. A user generating aflight plan to travel to waypoints associated with GCPs (e.g., asdescribed in FIG. 2 ), can indicate a ground sampling distance, which inthis specification identifies a lower acceptable threshold on imagepixels per distance. That is, the ground sampling distance identifiesthat in captured imagery, only imagery which includes at least thethreshold image pixels per distance (e.g., 3 pixels/cm) will beacceptable. Therefore, the user can designate the ground samplingdistance and altitude at which the UAV 4 is to travel at (e.g., the safealtitude 12), and a system being utilized by the user can determine aminimum size of the physical marker 22, or created mark 20.Alternatively, the user can designate the ground sampling distance,along with one or more physical markers that are available to beutilized, and the system can determine one or more maximum altitudes atwhich the UAV can travel.

Optionally, the physical marker 22 can include one or more electroniccomponents, such as sensors, to be used in actively determining a timeat which the UAV 4 is directly over the physical marker 22. The physicalmarker can include electronic circuitry with a GNSS receiver. Once thephysical marker is placed onto the surface, the physical marker mayobtain a geospatial position. The physical maker may have an identifierthat may be associated with the geospatial position. The geospatialposition of the maker and the identifier may be transmitted wirelesslyto the UAV, or to a ground control station.

Also, the physical marker may have wireless circuitry to transmit abeacon position, such as using BTLE (Bluetooth Low Energy). The markermay emit the beacon, which assists the UAV in obtaining a fix over thephysical maker. The UAV may receive the beacon from the physical markerand adjust the UAV position such that the UAV hovers to a fixed positionover the marker. In a near range position of the UAV in proximity to thephysical maker, the UAV could detect an accuracy of at least 30centimeters, or better. The physical maker could also have visiblemarkings, other non-visible markings in a different light spectrum (suchas ultra-violet, or infra-red) or LED lighting as discussed herein.

The physical marker can include a Bluetooth sensor that can provideinformation to the UAV 4 indicating when the UAV 4 is directly over acentroid of the physical marker 22. To determine when the UAV 4 isdirectly over the centroid, the physical marker 22 can include a laser,or other coherent optical source, that shines from the centroid, and theUAV 4 can include a reflective marker on the bottom at a location in avertical line with a GNSS receiver. Additionally, the physical marker 22can include sensors to determine the boundaries of the UAV 4 as ittravels over the physical marker 22, and can determine when theboundaries of the UAV 4 directly surround the centroid. The UAV 4 canobtain location information at a time the physical marker 22 indicatesit is over the centroid, for instance the UAV 4 can be continuously, orperiodically at a high frequency, obtaining location information whiletraveling at a threshold distance above the physical marker 22 (e.g.,the UAV 4 can move horizontally until receiving information from thephysical marker 22). The UAV 4 can then compare a timestamp of when thephysical marker 22 indicated the UAV 4 is over the centroid, to atimestamp associated with obtained location information. In this way,each physical marker 22 can include functionality for the UAV 4 todetermine its location, allowing off the shelf UAVs the ability toobtain location information of physical markers.

Optionally, each physical marker can include sensors, receivers,associated with ultra-wideband ranging, and can actively determinedistances between physical marker (e.g., sensors, receivers, can belocated at a centroid of a physical marker, or an offset can bedetermined from the centroid). These distances can be maintained (e.g.,by a cloud system as described below), such that distances between eachphysical marker can be stored and utilized (e.g., by a photogrammetrysystem). Consequently, the physical markers can be used as groundcontrol points in images, with a combined (e.g., stitched) imageutilizing scale information based on the distances between each physicalmarker (e.g. relative scale information, instead of precise locationinformation, can be determined from the combined image). For example,each physical marker can transmit time-pulses of a particular width(e.g., a short time-pulse to avoid multi-path interference), such thataccurate distance measurements can be made based on a time each pulsetraveled between the physical markers (e.g., time-of-flight measurementscan be performed between each physical marker, with clocks associatedwith the sensors synchronized using delay-locked loops). Optionally,each physical marker can include pattern information (e.g., as describedherein) on top of the physical marker, such that the physical marker canbe identified in images. Similarly, each physical marker can include aGNSS receiver (e.g., low-cost GNSS receiver), such that rough locationinformation for the receiver can be determined. Each physical marker canthen be identified in imagery using a location of a UAV that capturedthe imagery along with a field of view of the UAV. In this way, eachphysical marker can be identified, and distances between the physicalmarkers can be determined.

A frame may be used to house the physical markers 22 carried by the UAV.The UAV used with the frame ideally is a multi-copter UAV with at least3 arms extending from the body of the UAV. The UAV may have one motorand a rotor for each arm, or a coaxial configuration with two motorseach with a rotor. The frame ideally is constructed of a light weightmaterial, such as aluminum or carbon fiber. The frame can be attached tothe UAV on the body of the UAV. An actuator controlled by the UAVcomputer system may be used to release a physical marker.

In a third embodiment, the UAV 4 can obtain detailed imagery of asurface at the geographic location of the GCP using a camera 24, andobtain location information of a centroid of the imagery. The UAV 4 canbe trained to identify particular features (e.g., permanent features)that can opportunistically be utilized as GCPs. For instance, a manholecover 26 is a fixed object at a geographic location, and the UAV 4 cantravel to the manhole cover 26 (e.g., a user can identify the manholecover 26 in satellite imagery, and assign the manhole cover 26 as aGCP), and determine a centroid of the manhole cover 26. A non-exhaustivelist of objects, features, and so on, that can be utilized include firehydrants, mailboxes, signs, cable boxes, fixed features placed by agovernmental entity, and so on. These objects, features, and so on, canbe later identified in imagery captured by a UAV implementing asubsequent flight plan to perform a job, and thus used as GCPs.

Additionally, the UAV 4 can descend towards the surface, and determinewhether the surface includes sufficient identifying features, such thatthe features can be resolved by a camera included in a UAV performing asubsequent flight plan associated with a job. For instance, the UAV 4can determine that a surface which is mainly a same color (e.g., grass,cement, and so on), will not be suitable for later identification inimagery. In this instance, the UAV 4 can determine to create anidentifiable marker 20, or drop a physical marker 22. A user assigning,via the user device, geographic locations as GCPs can indicate that theUAV 4 is to prefer obtaining imagery, and if the surface does notinclude sufficient unique features, the UAV 4 is to create a mark, ordrop a marker.

The UAV 4 can determine quality information associated with the capturedimagery, and discard images that are blurry, not sharp, out of focus,and so on. Quality information about captured imagery can be determinedby sharpness measurements of the image. For instance, a frequency domainanalysis of the image can be performed, and a lack of high frequenciescan be indicative of a lack of focus (e.g., compared to an expectedinclusion of high frequencies for the image). Additionally, a laplaciankernel can be convolved with the image (e.g., in the spatial domain) andthe result can be used to determine blurriness of the image (e.g.,intensity values of pixels within a threshold distance can be compared,and a blurry image can have a lack of comparisons greater than athreshold). Additional quality information can include brightnessmeasurements, exposure measurements, contrast measurements, and so on.Optionally, the UAV 4 may have onboard GPU processing capabilities todetermine the quality information. The UAV 4 may after taking an image,move into a holding position, and the UAV 4 onboard processing system(e.g., described in FIG. 6 ) may analyze the image. If the onboardprocessing system determines that an image does not meet a thresholdquality, the UAV can then re-take the image. The UAV processing systemcan rerun the image quality review process, and can then continue withthe flight plan if the image passes the quality threshold. Furthermore,the UAV 4 can provide the captured imagery to a user device of anassociated operator for review (e.g., over a wireless connection), andthe operator can confirm or deny that the imagery is acceptable.

In the above embodiments in which the UAV 4 hovers while performing anaction, the UAV 4 can measure wind affecting the UAV 4 (e.g., using oneor more movement sensors such as accelerometers, rotational sensors, andso on, or one or more sensors that measure wind speed), and based on themeasured wind, the UAV 4 can wait to create a mark, or drop a physicalmarker, until a lull in the wind is determined. For instance, the UAV 4can determine that if the measure is less than a threshold (e.g., thewind is causing the UAV to not move more than a threshold horizontaland/or vertical distance, such that the UAV can remain stable, or thewind speed is less than a threshold), then the UAV 4 can place thephysical marker. If the wind begins to negatively affect the UAV 4 whileits creating a mark, the UAV 4 can pause the creation while it getsmoved around, and can return to creating the mark when the wind causesthe UAV 4 to remain substantially stable (e.g., not move in a directionmore than a threshold distance). The UAV 4 can monitor its preciselocation (e.g., using a RTK receiver, or by visually tracking a surfacethe UAV 4 is directly over, and use computer vision techniques asfeedback loops), and when a lull in the wind is detected, move to theprecise location at which it started creating the mark.

FIG. 1D illustrates an example diagram of a UAV 4 implementing a flightto perform a job. As illustrated, subsequent to the UAV 4 traveling toeach waypoint associated with a GCP, a flight plan to perform aparticular job can be implemented (e.g., by the same UAV 4, or adifferent UAV). In FIG. 1D, the UAV 4 is inspecting a rooftop of thehouse 6, and identifying damage (e.g., weather damage) to the rooftop.As illustrated, the UAV 4 has identified a portion 16 of the rooftop ofthe house 6 as being damaged, and is descending towards the portion 16while capturing imagery. Since the inspection area includes geographiclocations that have been designated as GCPs (e.g., sprayed with a fluid,a marker has been deposited on the geographic location), the capturedimagery can include one or more GCPs. In this way, the captured imagerycan be geo-rectified, and precise coordinate information can beobtained.

FIG. 2 illustrates an example user interface 200 for assigning groundcontrol points (GCPs) to geographic locations illustrated in imagery(e.g., satellite imagery). The user interface 200 is an example of aninteractive user interface that can be generated by a system (e.g., acloud system as described below) for presentation on a user device of auser. The user interface 200 can be an interactive document (e.g., a webpage) that the user device can receive over a network (e.g., theInternet), and render for presentation to the user. Optionally, the userinterface 200 can be generated by a user device of an operator proximateto a UAV that will be implementing a generated flight plan. The userdevice can receive assignments of GCPs, generate a flight plan, andprovide the flight plan to the UAV for implementation (e.g., live in thefield).

The user interface 200 can receive location information from the user,such as a particular address of a property to be inspected, longitudeand latitude coordinates, a neighborhood designation, and so on, and canpresent imagery (e.g., satellite imagery) that includes the location. Asillustrated in user interface 200, a house 202 is illustrated, alongwith neighboring streets and houses. Optionally, for implementations inwhich a user device of an operator generates a flight plan, or modifiesa generated flight plan as described in FIG. 1A-1B, the user device canobtain a present location of the user device (e.g., GNSS coordinates),and obtain imagery that includes the present location.

A user of the user interface 200 can assign GCPs to geographic locationswithin the presented imagery. For instance, the user has assignedgeographic locations 204A-204E as being GCPs, which are graphicallyillustrated in the user interface 200. The user can utilize the userinterface 200 to identify geographic locations that have been assignedas GCPs, and determine whether additional GCPs are to be assigned. Asdescribed above, the user can assign a greater density of GCPs to ageographic area that is proximate to an area of interest to the user.For example, as illustrated in the user interface 200, a particularhouse 202 is associated with a flight plan to perform a job (e.g.,identifying damage to a rooftop of the house 202, with the houseoutlined, or otherwise highlighted, to indicate the flight plan). Theuser has therefore assigned geographic locations proximate to the house202 as being GCPs, so that imagery captured of the house 202 can beproperly geo-rectified. In contrast, a single GCP 204C has been assignedat the upper edge of the user interface 200 since a lesser degree ofaccuracy is required at the upper edge.

The user interface 200 includes user selectable layers 206, that canshow a flight plan to perform a job and/or the Ground Control Pointsthat have been assigned. In the example of FIG. 2 , the flight plan hasnot been selected by the user, whereas the presently assigned GCPs layerhas been selected. The user can therefore view the geographic locationsassigned as GCPs. The user can interact with the layers 206 to show theflight plan to perform the job, and view waypoints, a flight pathbetween waypoints, and so on, that are associated with performing thejob. In this way the user can utilize the user interface 200 to ensurethat sufficient GCPs have been assigned.

While the GCPs may be selected by a user, the ground control stationsoftware, or a cloud-based system, may automatically designate groundcontrol points. The ground control station and cloud-based system mayanalyze an image of where an inspection will be performed. For example,these systems may have an application program or software, that analyzesthe images for appropriate locations of a GCP. Ideal locations would besidewalks, driveways or other detectable surfaces. These surfaces may bedetected based on known object detection techniques. Ideally, the groundcontrol point will be placed a location that is within a field of viewof a UAV sensor while the UAV is conducting an inspection. The systemsmay calculate a field of view area based on a field of view of a imagesensor, such as a digital camera, and an altitude of where the UAV willbe conducting an inspection. The system may select multiple groundcontrol point locations around, or within the field of view area. Theground control point locations may be presented via a user interface.The ground control points locations may optionally be moveable toanother location. For example, the system may analyze an image, anddetermine one or more suitable locations to place ground control points.A ground control point may be selected on a concrete sidewalk next to arooftop of a structure being selected. A user of the system may selectthe ground control point and move it to a different location.Additionally, the automatically generated ground control points mayoptionally be deleted by a user input. These automatically generatedground control points may be transmitted to a UAV as discussed herein.Also, the system may determine areas where a ground control point cannot be placed. For example, the system may detect based on a coloranalysis that a body of water, such as a pool or pond exists within thefield of view or inspection area. The system would avoid placing aground control points in these detected locations. The system mayoptionally be configured such that a user of the system may not be ableto place a ground control point in these detected locations. Based onobject detection, or colors of portions of the image, the system may beable to detectable usable or non-usable locations for placement ofground control points.

Each geographic location assigned as a GCP can be set as a particularwaypoint (e.g., as described above) for a UAV to travel to and designatethe geographic location as a GCP (e.g., mark the geographic location).In addition to setting waypoints, the user can interact with the userinterface 200 to indicate a type of action the UAV is to perform at eachwaypoint (e.g., creating a marker, dropping a marker, obtaining detailedimagery). The user interface 200 can access information describingcapabilities of UAVs that are available to be used (e.g., at aparticular time and/or geographic area), and can present only types ofactions that are possible with the capabilities of the UAVs (e.g., theuser may not have access to UAVs that can create markers). Furthermore,the user can designate a waypoint transition speed between eachwaypoint, and an altitude (e.g., a safe altitude) at which a UAV is totravel at between waypoints.

After entering GCP assignments, the user can interact with the userinterface 200 to generate a flight plan to be provided to a UAV toimplement traveling to each geographic location assigned as a GCP (e.g.,as described above). A system (e.g., a cloud system) can generate aflight plan, which can be provided to a user device of an operator fortransmission to the UAV, or to the UAV (e.g., over a wireless or wiredconnection).

Optionally, the flight plan can include both a flight plan to designategeographic locations as GCPs, but also the flight plan to perform thejob. In this way, the same UAV can perform both flight plans, with theperformance of the job immediately following the designation of GCPs.Optionally, the flight plans can be coordinated such that, the UAV candesignate GCPs in a particular geographic area, and perform the flightplan associated with the job in that same geographic area. Subsequently,the UAV can travel to a different geographic area and repeat theprocess. In this way, for flight plans that involve a large geographicarea, the overall time for completion can be shortened.

Optionally, the flight plan to designate geographic locations as GCPscan be performed by a first UAV, and a second UAV can perform the jobafter the first. As described above, for particular flight plans thatinclude a large geographic area, the second UAV can perform the flightplan associated with the job in a particular geographic area subsequentto the first UAV designating GCPs in the particular geographic area.

FIG. 3 illustrates a block diagram of an example cloud system 300. Thecloud system 300 can be a system of one or more computers, or softwareexecuting on a system of one or more computers. The cloud system 300 cangenerate flight plans 314 to be implemented by an unmanned aerialvehicle (UAV) to designate geographic locations as ground control points(GCPs), and obtain accurate location information (e.g., GPScoordinates), of each designated geographic location.

The cloud system 300 includes a flight plan generation engine 302 thatcan generate user interface data 306 for presentation on a user device310 (e.g., user interface 200 described above with respect to FIG. 2 )as user interfaces 316 configured to receive assignments of geographiclocations as GCPs. For instance, a user 330 can provide user input 332to a user interface 316 to indicate a location at which a flight plan isto take place (e.g., an address), and the user device 310, or cloudsystem 300, can obtain imagery (e.g., satellite imagery) of thelocation. The user 330 can then interact with the user interface 316 toassign particular geographic locations included in the imagery as GCPs.Subsequently, the flight planning generation engine 302 can generate aflight plan 314 for a UAV 320 to implement. The cloud system 300 canprovide the flight plan 314 to the UAV 320, or alternatively a userdevice (e.g., user device 310, or a user device of an operatorpositioned proximate to the entered location) can receive the flightplan 314, and provide the flight plan 314 to the UAV 320. Optionally,the flight plan generating engine 302 can analyze geographic locationsassigned by the user 330 (e.g. determine whether the placements shouldbe modified), and/or can determine geographic locations to be assignedas GCPs. The flight plan generation engine 302 can, for example,determine that GCPs are to evenly be distributed in the indicatedlocation (e.g., the engine 302 can determine that an even distributionprovides the greatest accuracy). Additionally, the flight plangeneration engine 302 can obtain information describing heights of asurface (e.g., the ground) in the indicated location (e.g., theinformation can be a topological map, a 3D model, a terrain model), andcan determine that additional GCPs are to be included in portions of thelocation with greater than a threshold height variance. The engine 302can receive (e.g., from the user 330) a minimum accuracy required, andcan utilize the minimum accuracy to inform a minimum number of GCPs thatare to be included in the location. Similarly, to maintain the minimumaccuracy in portions of the location in which heights of the surfacevary with greater than a threshold variance, the engine 302 candetermine that more GCPs are to be included (e.g., based on the minimumaccuracy and particular height variances). The engine 302 can optionallyreceive a maximum number of GCPs that can be created in the location(e.g., a maximum number of physical markers can be used), and candetermine locations to place the GCPs (e.g., based on height informationas described above) that will provide the greatest accuracy.

As described above, the UAV 320 can travel to waypoints associated withgeographic locations assigned as GCPs, and perform actions at eachwaypoint to designate the geographic location as a GCP (e.g., mark thegeographic location), and obtain accurate location information at thedesignated geographic location (e.g., location information at a centroidof the designated geographic location). The location information 326 canbe provided to the user device 310 (e.g., user device of an operator),and the cloud system 300 can receive the location information 326 andstore the information 326 in one or more databases 304.

In this way, imagery captured during a subsequent flight plan of a UAVto perform a job (e.g., an inspection of a property or structure fordamage) at the entered location can be utilized in conjunction with thestored location information 304 to generate geo-rectified imagery.

FIG. 4 is a flowchart of an example process 400 to designate real-worldgeographic locations as ground control points, and obtain locationinformation at the designated geographic locations. For convenience, theprocess 400 will be described as being performed by an unmanned aerialvehicle (UAV) that includes one or more processors (e.g., an unmannedaerial vehicle implementing the primary processing system 600).

The UAV receives a flight plan (block 402). As described above, a usercan assign geographic locations as ground control points (GCPs), and aflight plan can be generated with each assigned geographic locationbeing associated with a waypoint the UAV is to travel to. The UAV canreceive the flight plan from an operator (e.g. a human operator incommunication with the UAV over a wired or wireless connection who isproximate to the UAV), or from a cloud system that generates flightplans (e.g., the cloud system 300).

The UAV travels to an initial waypoint associated with a GCP (block404). The UAV obtains information identifying a geographic locationassociated with the waypoint (e.g., GPS coordinates), and travels to thewaypoint. As illustrated in FIG. 1A, the UAV can travel at a particularaltitude (e.g., a safe altitude) indicated in the received flight planthat is safe for the UAV to travel at within an inspection areaindicated in the flight plan. The UAV can travel to the waypoint at aparticular speed indicated in the flight plan, and upon reachingvertically above the initial waypoint, can descend towards the waypoint.

The UAV descends to a surface at a geographic location associated withthe waypoint, and performs an action to designate the geographiclocation as a GCP (block 406). After traveling to the waypoint, the UAVdescends in a vertical line towards the surface (e.g., towards theground, towards a surface of a structure or property, and so on). Afterdescending to a threshold distance above the surface, the UAV performsan action to designate the geographic area as being a GCP. Optionally,the UAV can land on the surface, so as place a marker as describedabove, with reference to FIG. 1C.

The UAV performs an action according to information indicated in thereceived flight plan, and as illustrated in FIG. 1C, the UAV can createan identifiable marker by spraying a fluid on the surface, the UAV canplace, or drop, a physical marker on the surface, or the UAV can obtaindetailed imagery of the surface (e.g., a manhole cover).

The UAV obtains, and stores, location information associated with thedesignated geographic area (block 406). As described above, withreference to FIG. 1C, the UAV obtains location information (e.g., GNSScoordinates) at a centroid of the designated geographic area. The UAVstores the location information, and optionally can provide the locationinformation to a user device of an operator (e.g., over a wirelessconnection).

The UAV provides the location information to a system for storage (block408). Subsequent to the UV traveling to each waypoint, the UAV providesthe location information, and optionally captured imagery of designatedgeographic locations as described in FIG. 1C, to an outside system(e.g., the cloud system 300) for storage. The location information canbe utilized when generating ortho-rectified or geo-rectified imageryfrom images that include geographic locations designated as GCPs.

FIGS. 5A-B illustrate example diagrams of an addition embodiment ofdesignating geographic locations as GCPs, and obtaining locationinformation associated with the designated geographic locations. Asdescribed above, with reference to FIGS. 1A-1D, a flight plan can begenerated that includes waypoints associated with geographic locationsassigned as GCPs. A user can assign geographic locations as GCPs, wherethe geographic locations can, in some implementations, be safelydescended to from a high altitude (e.g., there no obstructions that willinterfere with the UAV). To assign GCPs, the user can view imagery(e.g., satellite imagery) and identify geographic locations free ofobstructions. Additionally, an operator that travels to with the UAV canvisually determine whether obstructions exist, and update the flightplan to move one or more geographic locations.

In the Example of FIGS. 5A-5B, geographic locations can be assigned asGCPs, and a UAV can obtain location information associated with eachgeographic location without descending towards the surface.

FIG. 5A illustrates a vertical structure 502 (e.g., a cell tower) thatis connected with several guy-wires to a surface (e.g., the ground), andis proximate to several trees (e.g., trees 512 A-512 B). Each guy-wirecan be of a thickness that would make the guy-wire difficult to see insatellite imagery, and a user assigning geographic locations as GCPsmight assign a geographic location as being under, or too near, aguy-wire. Therefore, operator 504 can travel to the inspection area 508,and place physical markers 506 at geographic locations in the inspectionarea 508. That is, the operator 504 can determine geographic locationsto place GCPs, walk around and place on a surface the physical markers506 at the determined geographic locations. Optionally, a UAV can dropphysical markers as it travels at a particular altitude (e.g., a safealtitude as described in FIG. 1A), and optionally record locationinformation of each dropped physical marker. For instance, in large openclearings, it can be faster for a UAV to drop physical markers from thealtitude if the risk of humans being in danger of being hit by aphysical marker is low.

FIG. 5B illustrates an example diagram of a UAV 520 obtaining locationinformation associated with placed physical markers (e.g., physicalmarkers 506A-506C). The UAV 520 travels at a particular altitude (e.g.,a safe altitude as described in FIG. 1A) towards a physical marker(e.g., physical marker 506A).

When the operator places physical markers, the operator can optionallyobtain location information (e.g., GNSS coordinates from a consumergrade GNSS receiver) that indicates an approximate location of eachphysical marker. The UAV 520 can obtain information describing theapproximate locations of the physical markers, and set each approximatelocation as a waypoint to travel to. The UAV 520 can therefore travel atthe particular altitude until reaching the approximate area, and canidentify a physical marker 506A using a camera included in, or connectedto, the UAV 520. Optionally, the UAV 520 can store informationdescribing the physical marker, including a shape, color, pattern (e.g.,created using an active display visible on the physical marker asdescribed above), and so on, and use the information to identify thephysical marker.

Alternatively, the UAV 520 can travel within the inspection area 508,and identify physical markers within the inspection area. To increase aspeed at which the UAV can identify physical markers, the UAV 520 cantravel at a maximum altitude that still enables the UAV 520 to identifya physical marker on the surface. For instance, the maximum altitude canbe based on an acceptable ground sampling distance (e.g., an acceptablenumber of pixels per distance) for one or more visual recognitionalgorithms that can identify physical markers. Since the ground samplingdistance depends on capabilities of the camera (e.g., sensor size,sensor resolution, and so on as described above), a UAV with a bettercamera (e.g., greater resolution), can travel at a higher altitude toidentify physical markers.

The UAV 520 travels to a physical marker 506A, and hovers verticallyover the physical marker 506A. As described above, with respect to FIG.1C, the UAV 520 can determine a centroid of the physical marker 506Ausing a camera and information describing a shape, and/or color orpattern, of the physical marker 506A, and can obtain locationinformation at the centroid. Similar to FIG. 1C, the obtained locationinformation can be modified by an offset defined by a difference betweena horizontal difference in the center of the camera and a locationreceiver (e.g., GNSS receiver).

Optionally, the physical marker 506A can include, at the centroid, anarea that is reflective to particular wavelengths of electromagneticradiation. The UAV 520 can activate a sensor that provideselectromagnetic radiation, and maneuver the UAV 520 to increase areceived signal reflected from the physical marker 506A. In this way,the UAV 520 can accurately determine when it's located substantiallyover the centroid of the physical marker 506A (e.g., within a thresholddistance of a precise centroid). Since the sensor is likely to not be ina purely vertical line with the location receiver, the obtained locationinformation can be modified by a horizontal difference in the sensor andthe location receiver.

The UAV 520 travels vertically over each physical marker, and obtainslocation information. Subsequently, the UAV 520, or a different UAV, canperform a subsequent flight plan to perform a job. For instance, thevertical structure 502 can be inspected, and captured imagery of thevertical structure 502 can include the physical markers 506A-506C.

UAVs Acting in Concert

The above description includes methods and systems to designategeographic locations as GCPs, and obtain location information of thedesignated geographic locations. As described in FIG. 2 , a first UAVand a second UAV can act in concert, with the first UAV designatingGCPs, and the second UAV implementing a flight plan to perform a job.Optionally, the first UAV can include an identifiable marker facingvertically upwards, and act as a GCP in imagery captured by the secondUAV flying above the first UAV. For instance, the first UAV can includea display (e.g., an LED panel, one or more visual, infrared,ultraviolet, lights, and so on) utilized to display particular shapes,numbers, letters, and so on.

As described in FIG. 2 , the first and second UAVs can receive flightplans, with the first UAV implementing a flight plan to travel togeographic locations assigned as GCPs, and the second UAV implementing aflight plan to perform a job (e.g., inspecting an area for damage). Thefirst UAV can be positioned lower than the second UAV, and the secondUAV can capture imagery of the first UAV for use as a GCP. Optionally,both UAVs may be manually operated, or operated based on flight plans incommunication with each other, with the first UAV flown to and landingat a first location, and the second UAV flown above the first UAV toobtain images of the first UAV at a surface level

The first UAV and second UAV can act in concert (e.g., the first UAV canbe in communication with the second UAV), such that the first UAV isalways included in captured imagery of the second UAV. For instance, thesecond UAV can provide information to the first UAV indicating that it'sno longer visible by second UAV (e.g., no longer included in capturedimagery), and the first UAV can hover in place until the second UAV cansee it or is located directly over the first UAV, or can travel to alocation which is viewable by the second UAV. Additionally, the secondUAV can provide its present location along a flight path to the firstUAV, and the first UAV can ensure that it's below the second UAV.Additionally, the first UAV can provide information to the second UAVindicating a location (e.g., geospatial location indicated by GNSScoordinates) at which the first UAV is to travel. The second UAV canthen travel (e.g., navigate) to the location at an altitude a thresholddistance above the first UAV (e.g., the first UAV can land on asurface), and capture imagery that includes the first UAV.

The first UAV can record its location when it is at a location to beused as a ground control point, and can associate the recorded locationswith timestamps. When captured imagery is taken from the second UAVafter performance of the job, an outside system (e.g., a photogrammetrysystem), can correlate timestamps associated with the first UAVsrecorded locations with timestamps of when the second UAV capturedimages. In this way, the outside system can determine that, for aparticular image captured by the second UAV, the first UAV visible inthe image was located at a particular location.

However, since GCPs are generally assumed to be fixed on a surface(e.g., the ground) of a real-world coordinate frame, if the first UAV isnot substantially close to the surface in each image, the outside systemcan improperly generate ortho-rectified or geo-rectified imagery.Therefore, a projection from the first UAVs location in 3-D space can bemade to a location vertically down on the surface (e.g., the ground).That is, a location on the surface can be determined that is verticallybelow the first UAVs position in each captured image by the second UAV.Optionally, the first UAV can land on the surface, and the second UAVcan position itself directly over the first UAV and record locationinformation. The first UAV may transmit its geospatial location to thesecond UAV, and the second UAV use the location position, and at analtitude over the first UAV. An operator may use a ground controlstation to control both UAVs. The first UAV may transmit its geospatialposition to the ground control station, and the ground control stationmay transmit the first UAV position to the second UAV, and cause thesecond UAV to navigate to a position, and at an altitude over the firstUAV.

To effect this projection, the first UAV can additionally monitor, andrecord, altitude information at each timestamp associated with recordinglocation information. The first UAV can utilize a distance sensor (e.g.,a Lidar sensor, a Leddar sensor, barometric sensor) to accuratelydetermine its distance from the surface. The outside system can utilizethe distance, along with perspective information included in each image(e.g., determined from a field of view of a camera of the second UAV),to determine the projection.

In this way, the outside system can fix the first UAV to the surface,and properly generate geo-rectified or ortho-rectified imagery.

In a simpler manner, the first UAV can communicate geospatialinformation (e.g., GNSS coordinates) at which the first UAV is totravel. The second UAV can then travel to the location indicated by thereceived geospatial information, such that the first and second UAV canbe substantially in a vertical direction

Similarly, a vehicle can drive around within an inspection area thatincludes a location receiver (e.g., a GNSS receiver), and a visuallyidentifiable mark on top. A UAV implementing a flight plan to perform ajob can capture imagery that includes the vehicle, and an outside systemcan utilize the vehicle as a GCP in each image.

GCP Proxies

Known locations of fixed features can be utilized as GCPs while a UAVimplements a flight plan to perform a job. For instance, if the UAV isdetermining damage (e.g., weather damage) to the rooftop of the house, aGCP can be the corners of the property boundaries, or parcel thatincludes the house, if sufficiently accurate data for the corners can beobtained. Similarly, manhole covers, fire hydrants, and so on, can beutilized as GCPs if their locations have been previously determined.

FIG. 6 illustrates a block diagram of an example Unmanned Aerial Vehicle(UAV) architecture for implementing the features and processes describedherein. A UAV primary processing system 600 can be a system of one ormore computers, or software executing on a system of one or morecomputers, which is in communication with, or maintains, one or moredatabases. The UAV primary processing system 600 can be a system of oneor more processors 635, graphics processors 636, I/O subsystem 634,logic circuits, analog circuits, associated volatile and/or non-volatilememory, associated input/output data ports, power ports, etc., and/orone or more software processing executing one or more processors orcomputers. Memory 618 may include non-volatile memory, such as one ormore magnetic disk storage devices, solid state hard drives, or flashmemory. Other volatile memory such a RAM, DRAM, SRAM may be used fortemporary storage of data while the UAV is operational. Databases maystore information describing UAV flight operations, flight plans,contingency events, geofence information, component information, andother information.

The UAV processing system may be coupled to one or more sensors, such asGPS receivers 650, gyroscopes 656, accelerometers 658, pressure sensors(static or differential) 652, current sensors, voltage sensors,magnetometer, hydrometer, and motor sensors. The UAV may use an inertialmeasurement unit (IMU) 632 for use in navigation of the UAV. Sensors canbe coupled to the processing system, or to controller boards coupled tothe UAV processing system. One or more communication buses, such as aCAN bus, or signal lines, may couple the various sensor and components.

Various sensors, devices, firmware and other systems may beinterconnected to support multiple functions and operations of the UAV.For example, the UAV primary processing system 600 may use varioussensors to determine the vehicle's current geo-spatial location,attitude, altitude, velocity, direction, pitch, roll, yaw and/orairspeed and to pilot the vehicle along a specified route and/or to aspecified location and/or to control the vehicle's attitude, velocity,altitude, and/or airspeed (optionally even when not navigating thevehicle along a specific path or to a specific location).

The flight control module (also referred to as flight control engine)622 handles flight control operations of the UAV. The module interactswith one or more controllers 640 that control operation of motors 642and/or actuators 644. For example, the motors may be used for rotationof propellers, and the actuators may be used for flight surface controlsuch as ailerons, rudders, flaps, landing gear, and parachutedeployment.

The contingency module 624 monitors and handles contingency events. Forexample, the contingency module may detect that the UAV has crossed aborder of a geofence, and then instruct the flight control module toreturn to a predetermined landing location. Other contingency criteriamay be the detection of a low battery or fuel state, or malfunctioningof an onboard sensor, motor, or a deviation from the flight plan. Theforegoing is not meant to be limiting, as other contingency events maybe detected. In some instances, if equipped on the UAV, a parachute maybe deployed if the motors or actuators fail.

The mission module 629 processes the flight plan, waypoints, and otherassociated information with the flight plan. The mission module 629works in conjunction with the flight control module. For example, themission module may send information concerning the flight plan to theflight control module, for example lat/long waypoints, altitude, flightvelocity, so that the flight control module can autopilot the UAV.

The UAV may have various devices connected to it for data collection.For example, photographic camera 649, video cameras, infra-red camera,multispectral camera, and Lidar, radio transceiver, sonar, TCAS (trafficcollision avoidance system). Data collected by the devices may be storedon the device collecting the data, or the data may be stored onnon-volatile memory 618 of the UAV processing system 600.

The UAV processing system 600 may be coupled to various radios, andtransmitters 659 for manual control of the UAV, and for wireless orwired data transmission to and from the UAV primary processing system600, and optionally the UAV secondary processing system 602. The UAV mayuse one or more communications subsystems, such as a wirelesscommunication or wired subsystem, to facilitate communication to andfrom the UAV. Wireless communication subsystems may include radiotransceivers, and infrared, optical ultrasonic, electromagnetic devices.Wired communication systems may include ports such as Ethernet, USBports, serial ports, or other types of port to establish a wiredconnection to the UAV with other devices, such as a ground controlsystem, cloud-based system, or other devices, for example a mobilephone, tablet, personal computer, display monitor, other network-enableddevices. The UAV may use a light-weight tethered wire to a groundcontrol station for communication with the UAV. The tethered wire may beremoveably affixed to the UAV, for example via a magnetic coupler.

Flight data logs may be generated by reading various information fromthe UAV sensors and operating system and storing the information innon-volatile memory. The data logs may include a combination of variousdata, such as time, altitude, heading, ambient temperature, processortemperatures, pressure, battery level, fuel level, absolute or relativeposition, GPS coordinates, pitch, roll, yaw, ground speed, humiditylevel, velocity, acceleration, contingency information. This foregoingis not meant to be limiting, and other data may be captured and storedin the flight data logs. The flight data logs may be stored on aremovable media and the media installed onto the ground control system.Alternatively, the data logs may be wirelessly transmitted to the groundcontrol system or to the cloud system.

Modules, programs or instructions for performing flight operations,contingency maneuvers, and other functions may be performed with theoperating system. In some implementations, the operating system 620 canbe a real time operating system (RTOS), UNIX, LINUX, OS X, WINDOWS,ANDROID or other operating system. Additionally, other software modulesand applications may run on the operating system, such as a flightcontrol module 622, contingency module 624, application module 626, anddatabase module 628. Typically flight critical functions will beperformed using the UAV processing system 600. Operating system 620 mayinclude instructions for handling basic system services and forperforming hardware dependent tasks.

In addition to the UAV primary processing system 600, a secondaryprocessing system 602 may be used to run another operating system toperform other functions. A UAV secondary processing system 602 can be asystem of one or more computers, or software executing on a system ofone or more computers, which is in communication with, or maintains, oneor more databases. The UAV secondary processing system 602 can be asystem of one or more processors 694, graphics processors 692, I/Osubsystem 994 logic circuits, analog circuits, associated volatileand/or non-volatile memory, associated input/output data ports, powerports, etc., and/or one or more software processing executing one ormore processors or computers. Memory 670 may include non-volatilememory, such as one or more magnetic disk storage devices, solid statehard drives, flash memory. Other volatile memory such a RAM, DRAM, SRAMmay be used for storage of data while the UAV is operational.

Ideally modules, applications and other functions running on thesecondary processing system 602 will be non-critical functions innature, that is if the function fails, the UAV will still be able tosafely operate. In some implementations, the operating system 972 can bebased on real time operating system (RTOS), UNIX, LINUX, OS X, WINDOWS,ANDROID or other operating system. Additionally, other software modulesand applications may run on the operating system 672, such as anapplication module 974, database module 676. Operating system 602 mayinclude instructions for handling basic system services and forperforming hardware dependent tasks.

Also, controllers 646 may be used to interact and operate a payloaddevice 948, and other devices such as photographic camera 649, videocamera, infra-red camera, multispectral camera, stereo camera pair,Lidar, radio transceiver, sonar, laser ranger, altimeter, TCAS (trafficcollision avoidance system), ADS-B (Automatic dependentsurveillance-broadcast) transponder. Optionally, the secondaryprocessing system 602 may have coupled controllers to control payloaddevices.

Each of the processes, methods, and algorithms described in thepreceding sections may be embodied in, and fully or partially automatedby, code modules executed by one or more computer systems or computerprocessors comprising computer hardware. The code modules (or “engines”)may be stored on any type of, one or more, non-transitorycomputer-readable media (e.g., a computer storage product) or computerstorage devices, such as hard drives, solid state memory, optical disc,and/or the like. The systems and modules may also be transmitted asgenerated data signals (for example, as part of a carrier wave or otheranalog or digital propagated signal) on a variety of computer-readabletransmission mediums, including wireless-based and wired/cable-basedmediums, and may take a variety of forms (for example, as part of asingle or multiplexed analog signal, or as multiple discrete digitalpackets or frames). The processes and algorithms may be implementedpartially or wholly in application-specific circuitry. The results ofthe disclosed processes and process steps may be stored, persistently orotherwise, in any type of non-transitory computer storage such as, forexample, volatile or non-volatile storage.

In general, the terms “engine” and “module”, as used herein, refer tologic embodied in hardware or firmware, or to a collection of softwareinstructions, possibly having entry and exit points, written in aprogramming language, such as, for example, Java, Lua, C or C++. Asoftware module may be compiled and linked into an executable program,installed in a dynamic link library, or may be written in an interpretedprogramming language such as, for example, BASIC, Perl, or Python. Itwill be appreciated that software modules may be callable from othermodules or from themselves, and/or may be invoked in response todetected events or interrupts. Software modules configured for executionon computing devices may be provided on one or more computer readablemedia, such as a compact discs, digital video discs, flash drives, orany other tangible media. Such software code may be stored, partially orfully, on a memory device of the executing computing device. Softwareinstructions may be embedded in firmware, such as an EPROM. It will befurther appreciated that hardware modules may be comprised of connectedlogic units, such as gates and flip-flops, and/or may be comprised ofprogrammable units, such as programmable gate arrays or processors. Themodules described herein are preferably implemented as software modules,but may be represented in hardware or firmware. Generally, the modulesdescribed herein refer to logical modules that may be combined withother modules or divided into submodules despite their physicalorganization or storage.

User interfaces described herein are optionally presented (and userinstructions may be received) via a user computing device using abrowser, other network resource viewer, a dedicated application, orotherwise. Various features described or illustrated as being present indifferent embodiments or user interfaces may be combined into the sameembodiment or user interface. Commands and information received from theuser may be stored and acted on by the various systems disclosed hereinusing the processes disclosed herein. While the disclosure may referenceto a user hovering over, pointing at, or clicking on a particular item,other techniques may be used to detect an item of user interest. Forexample, the user may touch the item via a touch screen, or otherwiseindicate an interest. The user interfaces described herein may bepresented on a user terminal, such as a laptop computer, desktopcomputer, tablet computer, smart phone, virtual reality headset,augmented reality headset, or other terminal type. The user terminalsmay be associated with user input devices, such as touch screens,microphones, touch pads, keyboards, mice, styluses, cameras, etc. Whilethe foregoing discussion and figures may illustrate various types ofmenus, other types of menus may be used. For example, menus may beprovided via a drop down menu, a tool bar, a pop up menu, interactivevoice response system, or otherwise.

The various features and processes described above may be usedindependently of one another, or may be combined in various ways. Allpossible combinations and subcombinations are intended to fall withinthe scope of this disclosure. In addition, certain method or processblocks may be omitted in some implementations. The methods and processesdescribed herein are also not limited to any particular sequence, andthe blocks or states relating thereto can be performed in othersequences that are appropriate. For example, described blocks or statesmay be performed in an order other than that specifically disclosed, ormultiple blocks or states may be combined in a single block or state.The example blocks or states may be performed in serial, in parallel, orin some other manner. Blocks or states may be added to or removed fromthe disclosed example embodiments. The example systems and componentsdescribed herein may be configured differently than described. Forexample, elements may be added to, removed from, or rearranged comparedto the disclosed example embodiments.

Conditional language used herein, such as, among others, “can,” “could,”“might,” “may,” “for example,” and the like, unless specifically statedotherwise, or otherwise understood within the context as used, isgenerally intended to convey that certain embodiments include, whileother embodiments do not include, certain features, elements and/orsteps. Thus, such conditional language is not generally intended toimply that features, elements and/or steps are in any way required forone or more embodiments or that one or more embodiments necessarilyinclude logic for deciding, with or without author input or prompting,whether these features, elements and/or steps are included or are to beperformed in any particular embodiment. The terms “comprising,”“including,” “having,” and the like are synonymous and are usedinclusively, in an open-ended fashion, and do not exclude additionalelements, features, acts, operations, and so forth. Also, the term “or”is used in its inclusive sense (and not in its exclusive sense) so thatwhen used, for example, to connect a list of elements, the term “or”means one, some, or all of the elements in the list. Conjunctivelanguage such as the phrase “at least one of X, Y and Z,” unlessspecifically stated otherwise, is otherwise understood with the contextas used in general to convey that an item, term, etc. may be either X, Yor Z. Thus, such conjunctive language is not generally intended to implythat certain embodiments require at least one of X, at least one of Yand at least one of Z to each be present.

While certain example embodiments have been described, these embodimentshave been presented by way of example only, and are not intended tolimit the scope of the disclosure. Thus, nothing in the foregoingdescription is intended to imply that any particular element, feature,characteristic, step, module, or block is necessary or indispensable.Indeed, the novel methods and systems described herein may be embodiedin a variety of other forms; furthermore, various omissions,substitutions, and changes in the form of the methods and systemsdescribed herein may be made without departing from the spirit of theinventions disclosed herein. The accompanying claims and theirequivalents are intended to cover such forms or modifications as wouldfall within the scope and spirit of certain of the inventions disclosedherein.

Any process descriptions, elements, or blocks in the flow diagramsdescribed herein and/or depicted in the attached figures should beunderstood as potentially representing modules, segments, or portions ofcode which include one or more executable instructions for implementingspecific logical functions or steps in the process. Alternateimplementations are included within the scope of the embodimentsdescribed herein in which elements or functions may be deleted, executedout of order from that shown or discussed, including substantiallyconcurrently or in reverse order, depending on the functionalityinvolved, as would be understood by those skilled in the art.

It should be emphasized that many variations and modifications may bemade to the above-described embodiments, the elements of which are to beunderstood as being among other acceptable examples. All suchmodifications and variations are intended to be included herein withinthe scope of this disclosure. The foregoing description details certainembodiments of the invention. It will be appreciated, however, that nomatter how detailed the foregoing appears in text, the invention can bepracticed in many ways. As is also stated above, it should be noted thatthe use of particular terminology when describing certain features oraspects of the invention should not be taken to imply that theterminology is being re-defined herein to be restricted to including anyspecific characteristics of the features or aspects of the inventionwith which that terminology is associated.

While the disclosure has been described in connection with certainembodiments, it is to be understood that the disclosure is not to belimited to the disclosed embodiments but, on the contrary, is intendedto cover various modifications and equivalent arrangements includedwithin the scope of the appended claims, which scope is to be accordedthe broadest interpretation so as to encompass all such modificationsand equivalent structures as is permitted under the law.

What is claimed is:
 1. A computerized method comprising: receivinginformation describing a flight plan for an inspection of a propertyusing an unmanned aerial vehicle (UAV), the flight plan identifying oneor more waypoints proximate to the property; prior to the inspection ofthe property, for each of the one or more waypoints: navigating the UAVto the waypoint; placing, by the UAV, a physical marker onto a surfaceat the waypoint to form an identifiable mark on the surface; anddetermining a geographic location of the identifiable mark; andcapturing, using a camera of the UAV during the inspection of theproperty, images usable to generate rectified images associated with theinspection of the property based on the geographic locations of theidentifiable marks.
 2. The computerized method of claim 1, wherein thephysical marker includes fluid and placing the physical marker onto thesurface comprises: rotating a spray nozzle coupled to the UAV in acircular fashion while spraying the fluid onto the surface.
 3. Thecomputerized method of claim 1, wherein the physical marker includesfluid and placing the physical marker onto the surface comprises:spraying, by the UAV, the fluid in a first color onto the surface, andspraying, by the UAV, the fluid in a second color onto the surface. 4.The computerized method of claim 1, wherein the identifiable mark is apredetermined shape comprising one or more of a circle, x-pattern,sphere, or cross-hatch.
 5. The computerized method of claim 1, whereinthe UAV comprises one or more receptacles housing one or more fluidcontainers and one or more actuators coupled to the fluid containers. 6.The computerized method of claim 1, further comprising: providing thecaptured images and stored location information to a photogrammetrysystem for processing.
 7. The computerized method of claim 1, furthercomprising: receiving, via a user interface, input specifying selectionsof one or more locations; determining the flight plan for the UAV basedon the one or more locations; and transmitting, to the UAV, flightinformation including the flight plan via a wireless or wiredconnection.
 8. An apparatus, comprising: one or more processors; and oneor more non-transitory storage media storing instructions that, whenexecuted by the one or more processors, cause the one or more processorsto: receive information describing a flight plan for an inspection of aproperty using an unmanned aerial vehicle (UAV), the flight planidentifying one or more waypoints proximate to the property; prior tothe inspection, for each of the one or more waypoints: navigate the UAVto the waypoint; and place, by the UAV, a physical marker onto a surfaceat the waypoint to form an identifiable mark on the surface; andcapture, using a camera of the UAV during the inspection, images usableto generate rectified images associated with the inspection of theproperty based on geographic locations of the identifiable marks.
 9. Theapparatus of claim 8, wherein the physical marker includes fluid and theinstructions to place the physical marker onto the surface includeinstructions that, when executed by the one or more processors, causethe one or more processors to: rotate a spray nozzle coupled to the UAVin a circular fashion while spraying the fluid onto the surface.
 10. Theapparatus of claim 8, wherein the physical marker includes fluid and theinstructions to place the physical marker onto the surface includeinstructions that, when executed by the one or more processors, causethe one or more processors to: spray, by the UAV, the fluid in a firstcolor onto the surface; and spray, by the UAV, the fluid in a secondcolor onto the surface.
 11. The apparatus of claim 8, wherein theidentifiable mark is a predetermined shape comprising one or more of acircle, x-pattern, sphere or cross-hatch.
 12. The apparatus of claim 8,wherein the UAV comprises one or more receptacles housing one or morefluid containers and one or more actuators coupled to the fluidcontainers.
 13. The apparatus of claim 8, wherein the instructionsinclude instructions that, when executed by the one or more processors,cause the one or more processors to: provide the captured images andstored location information to a photogrammetry system for processing.14. The apparatus of claim 8, wherein the instructions includeinstructions that, when executed by the one or more processors, causethe one or more processors to: receive, via a user interface, inputspecifying selections of one or more locations; determine the flightplan for the UAV based on the one or more; and transmit, to the UAV,flight information including the flight plan via a wireless or wiredconnection.
 15. A non-transitory computer storage medium storinginstructions that, when executed by one or more processors, facilitate aperformance of operations, the operations comprising: receivinginformation describing a flight plan for an inspection of a propertyusing an unmanned aerial vehicle (UAV), the flight plan identifying oneor more waypoints; for each of the one or more waypoints: navigating theUAV to the waypoint; and placing, by the UAV, a physical marker onto asurface at the waypoint to form an identifiable mark on the surface; andcapture, using a camera of the UAV, images associated with theinspection of the property based on geographic locations of theidentifiable marks.
 16. The non-transitory computer storage medium ofclaim 15, wherein the physical marker includes fluid and the operationsfor placing the physical marker onto the surface include operationscomprising: rotating a spray nozzle coupled to the UAV in a circularfashion while spraying the fluid onto the surface.
 17. Thenon-transitory computer storage medium of claim 15, wherein the physicalmarker includes fluid and the operations for placing the physical markeronto the surface include operations comprising: spraying, by the UAV,the fluid in a first color onto the surface, and spraying, by the UAV,the fluid in a second color onto the surface.
 18. The non-transitorycomputer storage medium of claim 15, wherein the identifiable mark is apredetermined shape comprising one or more of a circle, x-pattern,sphere, or cross-hatch.
 19. The non-transitory computer storage mediumof claim 15, the operations further comprising: providing the capturedimages and stored location information to a photogrammetry system forprocessing.
 20. The non-transitory computer storage medium of claim 15,the operations further comprising: receiving, via a user interface,input specifying selections of one or more locations; determining theflight plan for the UAV based on the one or more locations; andtransmitting, to the UAV, flight information including the flight planvia a wireless or wired connection.